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Table 2 Verification of aerodynamic parameters for convergence of aerodynamic grids

From: Experimental design for a novel co-flow jet airfoil

Conditions

\(C_l\)

\(C_d\)

Con. 1

Con. 2

Con. 3

Con. 1

Con. 2

Con. 3

Grids

      

   Grid 1 (−20%)

1.0287

1.5215

2.0317

−0.00263

−0.00243

−0.00219

   Grid 1

1.0291

1.5218

2.0319

−0.00258

−0.00239

−0.00224

   Grid 1 (+20%)

1.0293

1.5221

2.0320

−0.00257

−0.00237

−0.00224